A smart embedded control unit for electro-hydraulic aircraft actuators

Marco Carminati, Matteo Rubagotti, Riccardo Grassetti, Giorgio Ferrari, Marco Sampietro

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

The design and experimental characterization of a novel electronic control unit for fly-by-wire aircraft actuators are presented. Thanks to a carefully-engineered compact volume, it is embedded in the actuator body, providing local closed-loop control. Various digital control laws can be implemented in the easily reconfigurable digital platform. After system modeling and tuning, a variable-gain controller has been selected. Beyond reduction of weight (900g), power dissipation (7W) and cabling connections (required only for power supply and digital communication bus), the advantages provided by this smart unit are both in terms of performance and safety improvement. In fact, fast (1Hz) and precise (1mm resolution, 2mm accuracy, no overshoot) closed-loop linear displacement regulation is here demonstrated. Furthermore, this robust and rugged unit is endowed with self-diagnostic capabilities: fault detection of all critical electronic and electro/mechanical sections is implemented by dedicated analog circuits. It is suitable for fully-electrical and hybrid electro-hydraulic actuators. Extensive thermal characterization has confirmed the fulfillment of specifications over the whole -40°C ÷ +70°C operating range.

Original languageEnglish
Title of host publicationInternational Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010
DOIs
Publication statusPublished - Dec 1 2010
EventInternational Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010 - Bologna, Italy
Duration: Oct 19 2010Oct 21 2010

Publication series

NameInternational Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010

Conference

ConferenceInternational Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010
CountryItaly
CityBologna
Period10/19/1010/21/10

Fingerprint

Actuators
Aircraft
Hydraulics
Hydraulic actuators
Analog circuits
Fault detection
Energy dissipation
Tuning
Wire
Specifications
Controllers
Communication
Hot Temperature

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

Cite this

Carminati, M., Rubagotti, M., Grassetti, R., Ferrari, G., & Sampietro, M. (2010). A smart embedded control unit for electro-hydraulic aircraft actuators. In International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010 [5665217] (International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010). https://doi.org/10.1109/ESARS.2010.5665217

A smart embedded control unit for electro-hydraulic aircraft actuators. / Carminati, Marco; Rubagotti, Matteo; Grassetti, Riccardo; Ferrari, Giorgio; Sampietro, Marco.

International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010. 2010. 5665217 (International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Carminati, M, Rubagotti, M, Grassetti, R, Ferrari, G & Sampietro, M 2010, A smart embedded control unit for electro-hydraulic aircraft actuators. in International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010., 5665217, International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010, International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010, Bologna, Italy, 10/19/10. https://doi.org/10.1109/ESARS.2010.5665217
Carminati M, Rubagotti M, Grassetti R, Ferrari G, Sampietro M. A smart embedded control unit for electro-hydraulic aircraft actuators. In International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010. 2010. 5665217. (International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010). https://doi.org/10.1109/ESARS.2010.5665217
Carminati, Marco ; Rubagotti, Matteo ; Grassetti, Riccardo ; Ferrari, Giorgio ; Sampietro, Marco. / A smart embedded control unit for electro-hydraulic aircraft actuators. International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010. 2010. (International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010).
@inproceedings{2e0027c7a80a49fc8d63806368b0d2a3,
title = "A smart embedded control unit for electro-hydraulic aircraft actuators",
abstract = "The design and experimental characterization of a novel electronic control unit for fly-by-wire aircraft actuators are presented. Thanks to a carefully-engineered compact volume, it is embedded in the actuator body, providing local closed-loop control. Various digital control laws can be implemented in the easily reconfigurable digital platform. After system modeling and tuning, a variable-gain controller has been selected. Beyond reduction of weight (900g), power dissipation (7W) and cabling connections (required only for power supply and digital communication bus), the advantages provided by this smart unit are both in terms of performance and safety improvement. In fact, fast (1Hz) and precise (1mm resolution, 2mm accuracy, no overshoot) closed-loop linear displacement regulation is here demonstrated. Furthermore, this robust and rugged unit is endowed with self-diagnostic capabilities: fault detection of all critical electronic and electro/mechanical sections is implemented by dedicated analog circuits. It is suitable for fully-electrical and hybrid electro-hydraulic actuators. Extensive thermal characterization has confirmed the fulfillment of specifications over the whole -40°C ÷ +70°C operating range.",
author = "Marco Carminati and Matteo Rubagotti and Riccardo Grassetti and Giorgio Ferrari and Marco Sampietro",
year = "2010",
month = "12",
day = "1",
doi = "10.1109/ESARS.2010.5665217",
language = "English",
isbn = "9781424490943",
series = "International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010",
booktitle = "International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010",

}

TY - GEN

T1 - A smart embedded control unit for electro-hydraulic aircraft actuators

AU - Carminati, Marco

AU - Rubagotti, Matteo

AU - Grassetti, Riccardo

AU - Ferrari, Giorgio

AU - Sampietro, Marco

PY - 2010/12/1

Y1 - 2010/12/1

N2 - The design and experimental characterization of a novel electronic control unit for fly-by-wire aircraft actuators are presented. Thanks to a carefully-engineered compact volume, it is embedded in the actuator body, providing local closed-loop control. Various digital control laws can be implemented in the easily reconfigurable digital platform. After system modeling and tuning, a variable-gain controller has been selected. Beyond reduction of weight (900g), power dissipation (7W) and cabling connections (required only for power supply and digital communication bus), the advantages provided by this smart unit are both in terms of performance and safety improvement. In fact, fast (1Hz) and precise (1mm resolution, 2mm accuracy, no overshoot) closed-loop linear displacement regulation is here demonstrated. Furthermore, this robust and rugged unit is endowed with self-diagnostic capabilities: fault detection of all critical electronic and electro/mechanical sections is implemented by dedicated analog circuits. It is suitable for fully-electrical and hybrid electro-hydraulic actuators. Extensive thermal characterization has confirmed the fulfillment of specifications over the whole -40°C ÷ +70°C operating range.

AB - The design and experimental characterization of a novel electronic control unit for fly-by-wire aircraft actuators are presented. Thanks to a carefully-engineered compact volume, it is embedded in the actuator body, providing local closed-loop control. Various digital control laws can be implemented in the easily reconfigurable digital platform. After system modeling and tuning, a variable-gain controller has been selected. Beyond reduction of weight (900g), power dissipation (7W) and cabling connections (required only for power supply and digital communication bus), the advantages provided by this smart unit are both in terms of performance and safety improvement. In fact, fast (1Hz) and precise (1mm resolution, 2mm accuracy, no overshoot) closed-loop linear displacement regulation is here demonstrated. Furthermore, this robust and rugged unit is endowed with self-diagnostic capabilities: fault detection of all critical electronic and electro/mechanical sections is implemented by dedicated analog circuits. It is suitable for fully-electrical and hybrid electro-hydraulic actuators. Extensive thermal characterization has confirmed the fulfillment of specifications over the whole -40°C ÷ +70°C operating range.

UR - http://www.scopus.com/inward/record.url?scp=78650943310&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=78650943310&partnerID=8YFLogxK

U2 - 10.1109/ESARS.2010.5665217

DO - 10.1109/ESARS.2010.5665217

M3 - Conference contribution

SN - 9781424490943

T3 - International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010

BT - International Conference on Electrical Systems for Aircraft, Railway and Ship Propulsion, ESARS 2010

ER -